# Service difficulty reports: N505MC, cancelled Nov 29, 2010 A list on [N505MC, cancelled Nov 29, 2010](https://openairdocs.org/deregistered/N505MC-2010-11-29.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 3 · 106 reports - [SDR UIEA200800151](https://openairdocs.org/sdr/UIEA200800151.md): Panel · damaged · Apr 15, 2008 · N505MC · Boeing 7472D3B · Wing, Plate/Skin > LT WING UPPER SURFACE NR 5 SPOILER CENTER HINGE GAP PANEL DAMAGED, ALSO, INBOARD, OUTBOARD AND CENTER HINGE CUT-OUT AND FORWARD PANEL OF CENTER HINGE DAMAGED, SKIN PULLED AND CRACKED. PERMANENT REPAIRS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG. 2, SHEETS - [SDR UIEA200800150](https://openairdocs.org/sdr/UIEA200800150.md): Panel · delaminated · Apr 15, 2008 · N505MC · Boeing 7472D3B · Wing, Plate/Skin > RT WING UPPER FIXED TRAILING EDGE PANEL, OUTBOARD OF NR 8 SPOILER HAS AN AREA OF 5.0 INCH BY 2.0 INCH OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 2, SHEETS 1, 2 AND 5. PREPREG LAYUP 250 DEGREES F CURE PER SRM 51-40-12. RE - [SDR UIEA200800149](https://openairdocs.org/sdr/UIEA200800149.md): Skin · cracked · Apr 15, 2008 · N505MC · Boeing 7472D3B · Passenger/Crew Doors > MAIN ENTRY DOOR L-1 EXTERIOR SKIN, UPPER HINGE CUT-OUT PREVIOUS DOUBLER REPAIR, LOWER RADIUS CORNER IS CRACKED. VERIFIED CRACK WITH HFEC AS PER B747-200 NDT MANUAL PART 6, 51-00-00 FIG 23. STOPPED DRILLED CRACK AND ACCOMPLISHED PERMANENT REPAIRS AS PER B747 - [SDR UIEA200800099](https://openairdocs.org/sdr/UIEA200800099.md): Lead · chafed · Apr 1, 2008 · N505MC · Boeing 7472D3B · Engine Indicating System Wiring > REJECTED TAKEOFF, NR 3 EGT WENT TO OFF SCALE HIGH WITH RED BALL. NR 3 ENGINE EGT SHOWED 1074 DEGREES FOR 1 SEC. FOUND THERMOCOUPLE LEAD WAS DEFECTIVE WHILE PERFORMING FIM PROCEDURE 71-03-00 AS NOTED IN AMM 72-00-00 PAGE 680G. REPLACED LEAD PER AMM 77-21-02 - [SDR UIEA200700467](https://openairdocs.org/sdr/UIEA200700467.md): Panel · delaminated · Nov 2, 2007 · N505MC · Boeing 7472D3B · Wing, Plate/Skin > LT WING UPPER L/E FIXED PANEL BETWEEN AISLES 170.0 TO AISLES 630.72 HAS AN AREA DELAMINATION, AREA IS 58.0 INCH LONG BY 50.0 INCH WIDE. INTERIM REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-16 AND ATLAS AIR EO NR 4757A402 PART 4. PER FAA FORM 8110-3 REQU - [SDR UIEA200700465](https://openairdocs.org/sdr/UIEA200700465.md): Panel · delaminated · Oct 26, 2007 · N505MC · Boeing 7472D3B · Wing, Plate/Skin > UPPER SURFACE OF LEFT WING INBOARD NR 2 ENGINE FIBERGLASS HAS HOLE AND DENT. REPAIRED PER XEO 57-102607 TRANS TO NON MEL N07-126. REINSPECTED IN ORD AND ACCOMPLISHED XEO 57-102607 PART 3 IAW SRM 51-40-16. REPAIRED AND TO BE INSPECTED EVERY 10 FLIGHT CYCLES - [SDR UIEA200700432](https://openairdocs.org/sdr/UIEA200700432.md): Sensor · failed · Oct 3, 2007 · N505MC · Boeing 7472D3B · Stall Warning System > AIR TURN BACK, AT ROTATION STICK SHAKER CAME ON AND STAYED ON UNTIL LANDING. VR SPEED WAS 129 KNOTS. REMOVED AND REPLACED LEFT AOA SENSOR AND STALL WARNING COMPUTER IAW 27-30-01, OPS CHECKED NORMAL IAW 27-30-00. - [SDR UIEA200700427](https://openairdocs.org/sdr/UIEA200700427.md): Skin · torn · Oct 1, 2007 · N505MC · Boeing 7472D3B · Elevator, Plate/Skin > LT INBOARD ELEVATOR, TRAILING EDGE COMPOSITE SKIN TIP AREA HAD GROUND DAMAGE. PERMANENT REPAIR ACCOMPLISHED AS PER B747 SRM 51-40-09, FIG 1A, SHEET 1 AND FIG 8, SHEETS 1 AND 2. REFERENCE ATLAS AIR EO NR 4755A049. - [SDR UIEA200700425](https://openairdocs.org/sdr/UIEA200700425.md): Skin · damaged · Oct 1, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Plate/Skin > LOWER AFT FUSELAGE EXTERIOR SKIN DOUBLER/TRIPLER AT FS 2613 PREVIOUS REPAIR DAMAGED WITH HEAVY ABRASION/SCRAPING DUE TO TAIL DRAG. REMOVED AND REPLACED DOUBLER/TRIPLER REPAIR AS PER 747-200 SRM 51-30-02 AND 51-30-03 FIG 1 SHEETS 1 THRU 6. REFERENCE ATLAS XEO - [SDR UIEA200700422](https://openairdocs.org/sdr/UIEA200700422.md): Skin · damaged · Oct 1, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Plate/Skin > FUSELAGE TAIL CONE LOWER AREA FROM FS 2742 TO 2792 SKIN AND FRAMES SCRAPED AND DENTED DUE TO TAIL DRAG. REMOVE AND REPLACED LOWER SECTION OF CONE FROM STA 2742 TO 2792, ASSY P/N 65B02785-1 AND PERMANENT REPAIRS ACCOMPLISHED AS PER B747-200 SRM 51-20-01 FIG 3, - [SDR UIEA200700426](https://openairdocs.org/sdr/UIEA200700426.md): Skin · damaged · Oct 1, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Plate/Skin > LOWER AFT FUSELAGE EXTERIOR SKIN DOUBLER/TRIPLER AT FS 2594 TO 2604.0 PREVIOUS REPAIR DAMAGED WITH HEAVY ABRASION/SCRAPING DUE TO TAIL DRAG. REMOVED AND REPLACED DOUBLER/TRIPLER REPAIR AS PER 747-200 SRM 51-30-02 AND 51-30-03 FIG 1 SHEETS 1 THRU 6. REFERENCE - [SDR UIEA200700424](https://openairdocs.org/sdr/UIEA200700424.md): Frame · damaged · Oct 1, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Frame > AFT LOWER FUSELAGE AT FS 2658 FRAME LOWER SURFACE SCRAPED DUE TO TAIL DRAG. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 53-10-04 FIG 75 SHEETS 1 THRU 15. REFERENCE ATLAS AIR XEO 53-093007. - [SDR UIEA200700423](https://openairdocs.org/sdr/UIEA200700423.md): Frame · damaged · Oct 1, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Frame > AFT LOWER FUSELAGE AT FS 2638 FRAME LOWER SURFACE SCRAPED DUE TO TAIL DRAG. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-20-01 FIG 3, AND SRM 51-30-02. ALSO REFERENCE ATLAS AIR XEO NR 53-093007-1. - [SDR UIEA200700145](https://openairdocs.org/sdr/UIEA200700145.md): Wire · chafed · Mar 26, 2007 · N505MC · Boeing 7472D3B · Fire Protection System Wiring > AFTER T/O FROM AMS, WHERE NR 3 ENGINE B LOOP WAS DEFERRED AS INOP. NR 3 ENGINE FIRE BELL AND LIGHT ILLUMINATED, NR 3 ENGINE A LOOP WAS ERRATIC AND WAS AT 10 ON THE SCALE FLUCTUATING. ENGINE SHUT DOWN AS PER ATLAS PROCEDURE USING FIRE CHECK LIST FIRE SWITCH A - [SDR UIEA200700130](https://openairdocs.org/sdr/UIEA200700130.md): Strap · cracked · Mar 4, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Structure > CRACKS FOUND ON BS 800 LT STRAP AND INNER CHORD AT NR 2 MAIN ENTRY DOOR. REPAIRED ACCOMPLISHED IAW SR ID NR 1-289052431 AND FAA FORM 8100-9. - [SDR UIEA200700125](https://openairdocs.org/sdr/UIEA200700125.md): Skin · corroded · Mar 2, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Plate/Skin > M/DECK RT NR 3 MED CUTOUT AFT UPPER CORNER SKIN STA1319, STR 17R-18R FOUND CORRODED. REPAIRED ACCOMPLISHED AS PER BOEING MESSAGE NR 1-289657194-1, 747 SRM 53-30-03 FIG 44 AND FAA FORM 8100-9. - [SDR UIEA200700128](https://openairdocs.org/sdr/UIEA200700128.md): Doubler · separated · Mar 2, 2007 · N505MC · Boeing 7472D3B · Wing, Plate/Skin > NR 3 PYLON FWD FIXED FAIRING LT EXTERIOR SURFACE AFT CORNER SKIN DOUBLER SEPARATED. FAIRING REPLACED BUT NUMEROUS FASTENERS HOLES FOUND MISALIGNED. TIME LIMIT REPAIRED ACCOMPLISHED AS PER BOEING MESSAGE NR 1-292185930-1 THRU -14, DWG 65B90813-52 AND FAA FORM - [SDR UIEA200700124](https://openairdocs.org/sdr/UIEA200700124.md): Bulkhead · corroded · Mar 2, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Bulkhead > BS 1250, L WLG W/W CANTED PRESSURE BULKHEAD, NR 2 PACK COOLING DUCT CUTOUT FOUND CORROSION. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-289645346-1 THRU -5 AND FAA FORM 8100-9. - [SDR UIEA200700129](https://openairdocs.org/sdr/UIEA200700129.md): Skin · corroded · Mar 2, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Plate/Skin > FOUND M/DECK STA1241 FRAME AND SKIN SPLICE AREA HAS HOLE, CRACKED AND CORRODED. REPAIRED ACCOMPLISHED AS PER BOEING MESSAGE NR 1-29020776-1 AND -6 AND FAA FORM 8100-9. - [SDR UIEA200700127](https://openairdocs.org/sdr/UIEA200700127.md): Stringer · corroded · Mar 2, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Longeron/Stringer > FWD CARGO COMPARTMENT STA 978, STR 47L FOUND CORRODED. FWD CARGO COMPARTMENT STA978, STR47L REPLACED AS PER SRM 51-10-01. - [SDR UIEA200700126](https://openairdocs.org/sdr/UIEA200700126.md): Intercostal · cracked · Mar 2, 2007 · N505MC · Boeing 7472D3B · Fuselage Miscellaneous Structure > UPPER DECK FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 420, LBL 50. U/DECK FLOOR SUPPORT INTERCOSTAL AT BS420, LBL 50 REPLACED AS PER SRM 51-30-02. - [SDR UIEA200700107](https://openairdocs.org/sdr/UIEA200700107.md): Stringer · cracked · Mar 1, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Longeron/Stringer > M/DECK ZONE "C" LT SIDEWALL STRUCTURE STA 905, STR-10L FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER SRM 53-10-03, FIG 4. - [SDR UIEA200700106](https://openairdocs.org/sdr/UIEA200700106.md): Keelbeam · bulged · Mar 1, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Keel > FOUND KEEL BEAM BOTH SIDES WEB BULGE FOUND AT BS 1450. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-286690602-1 THRU -10. - [SDR UIEA200700101](https://openairdocs.org/sdr/UIEA200700101.md): Shear Tie · cracked · Feb 28, 2007 · N505MC · Boeing 7472D3B · Fuselage Internal Mounting Structure > RT STA 840 FWD CHANNEL TENSION TIE AT 12 O'CLOCK FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID 1-288425027-1 AND -6, 1-289012875-1, SB747-53-2502 AND FAA FORM 8100-9. - [SDR UIEA200700100](https://openairdocs.org/sdr/UIEA200700100.md): Skin · cracked · Feb 28, 2007 · N505MC · Boeing 7472D3B · Nacelle/Pylon, Plate/Skin > NR 3 ENGINE LT CORE COWL SKIN BOND DOUBLER CRACKED AT AIR EXHAUST DUCT AFT LOWER PORTION. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-286833874-1 THRU -6, DWG 65B94280 AND FAA FORM 8100-9. - [SDR UIEA200700099](https://openairdocs.org/sdr/UIEA200700099.md): Skin · punctured · Feb 28, 2007 · N505MC · Boeing 7472D3B · Trailing Edge Flaps > NR 20 VC FLAP FOLDING NOSE I/B END SKIN PUNCHED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-290202458-1 THRU -3 AND FAA FORM 8100-9. - [SDR UIEA200700098](https://openairdocs.org/sdr/UIEA200700098.md): Stringer · cracked · Feb 28, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Longeron/Stringer > M/DECK LT SIDE STA 875, STR9L FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03, FIG.4 - [SDR UIEA200700097](https://openairdocs.org/sdr/UIEA200700097.md): Crease Beam · cracked · Feb 28, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Structure > M/DECK RTH SIDE STA 940, S-8R CREASE BEAM WEB FOUND CRACKED. CREASE BEAM WEB REPLACED AS PER SRM 51-10-01 AND 51-30-02. - [SDR UIEA200700096](https://openairdocs.org/sdr/UIEA200700096.md): Stringer · corroded · Feb 28, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Longeron/Stringer > FOUND FWD CARGO COMPT STA 980, STR 43R IS CORRODED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. - [SDR UIEA200700095](https://openairdocs.org/sdr/UIEA200700095.md): Crease Beam · cracked · Feb 28, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Structure > FOUND M/DECK STA960, S-7R CREASE BEAM SUPPORT ANGLE FOUND CRACKED. CREASE BEAM SUPPORT WEB REPLACED AS PER SRM 51-10-01. - [SDR UIEA200700094](https://openairdocs.org/sdr/UIEA200700094.md): Stringer · cracked · Feb 28, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Longeron/Stringer > M/DECK STA 895 STR 7R FOUND CRACKED. STRINGER REPAIRED ACCOMPLISHED AS PER SRM 53-10-03 FIG 4. - [SDR UIEA200700093](https://openairdocs.org/sdr/UIEA200700093.md): Skin · misrepaired · Feb 27, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Plate/Skin > FUSELAGE BS 690 S31L HAS 14" BY 12" EXTERNAL DOUBLER TO LT UPPER STATIC PORT PREVIOUS REPAIRED PER SRM 51-70-00 PG 8E AND F FIG 3 SHEET 6 AND 7. THIS REPAIR IS BEYOND THE LIMIT. REPAIRED ACCOMPLISHED AS PER SRM 53-30-03 FIG 1 AND 51-70-00 FIG 3. - [SDR UIEA200700090](https://openairdocs.org/sdr/UIEA200700090.md): Skin · cracked · Feb 26, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERNAL DOUBLER FOUND CRACKED AT NLG LT FWD CORNER. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-290193820-1 THRU -5 AND FAA FORM 8100-9. - [SDR UIEA200700086](https://openairdocs.org/sdr/UIEA200700086.md): Mount · damaged · Feb 25, 2007 · N505MC · Boeing 7472D3B · Engine Mount Section > NR 4 PYLON FWD ENGINE MOUNT FITTING BOTH I/B AND O/B LUG BORE HOLES FOUND OVERSIZED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-290193672-1 THRU -3 AND FAA FORM 8100-9. - [SDR UIEA200700089](https://openairdocs.org/sdr/UIEA200700089.md): Web · corroded · Feb 25, 2007 · N505MC · Boeing 7472D3B · Fuselage Miscellaneous Structure > FOUND LT WLG BS 1350 HORIZONTAL WEB UPPER SURFACE FOUND CORROSION. CORROSION REMOVED AND AREA PROTECTED AS PER SRM 51-10-01 AND 51-10-02. - [SDR UIEA200700085](https://openairdocs.org/sdr/UIEA200700085.md): Access Door · damaged · Feb 25, 2007 · N505MC · Boeing 7472D3B · Engine Thrust Reverser > NR 3 ENGINE RT FAN T/REV ACCESS DOOR ASSY SKIN DAMAGED. REPAIRED ACCOMPLISHED AS PER EO NR 4778A095 AND FAA FORM 8110-3. - [SDR UIEA200700087](https://openairdocs.org/sdr/UIEA200700087.md): Skin · cracked · Feb 25, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Plate/Skin > FUSELAGE SKIN BS 570 EQUIPMENT COOLING OUTLET FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER SB747-53-2386 FIG 5 AND 10. - [SDR UIEA200700088](https://openairdocs.org/sdr/UIEA200700088.md): Fairing · cracked · Feb 25, 2007 · N505MC · Boeing 7472D3B · Engine Thrust Reverser > ENGINE NR 2 RT T/REV AFT UPPER BEAVER TAIL FAIRING ASSY INNER SKIN FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER EO NR 4778A094 AND FAA FORM 8110-3. - [SDR UIEA200700083](https://openairdocs.org/sdr/UIEA200700083.md): Skin · corroded · Feb 22, 2007 · N505MC · Boeing 7472D3B · Wing, Plate/Skin > RIGHT WING UPPER SURFACE WS 697, STR28R AT FRONT SPAR FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM 51-10-01 AND 51-10-02. - [SDR UIEA200700084](https://openairdocs.org/sdr/UIEA200700084.md): Skin · corroded · Feb 22, 2007 · N505MC · Boeing 7472D3B · Wing, Plate/Skin > LEFT WING UPPER WING SKIN AT WS320, STR 14L-14L FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM 51-10-01 AND 51-10-02. - [SDR UIEA200700082](https://openairdocs.org/sdr/UIEA200700082.md): Skin · dented · Feb 22, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Plate/Skin > FUSELAGE SKIN DENT FOUND AT BS 1810, S51L-S51R. DENT AREA REWORKED AND PROTECTED AS PER SRM 51-40-01 AND 51-10-02. - [SDR UIEA200700081](https://openairdocs.org/sdr/UIEA200700081.md): Skin · corroded · Feb 22, 2007 · N505MC · Boeing 7472D3B · Wing, Plate/Skin > FOUND RIGHT WING UPPER SURFACE RWS642 AT MID SPAR FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM51-10-01 AND 51-10-02. - [SDR UIEA200700080](https://openairdocs.org/sdr/UIEA200700080.md): Skin · corroded · Feb 22, 2007 · N505MC · Boeing 7472D3B · Wing, Plate/Skin > FOUND LEFT WING UPPER WING SKIN AT WS 1280 FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM 51-10-01 AND 51-10-02. - [SDR UIEA200700075](https://openairdocs.org/sdr/UIEA200700075.md): Shear Web · cracked · Feb 21, 2007 · N505MC · Boeing 7472D3B · Fuselage Miscellaneous Structure > TENSION TIE BS 840-BS 860, LT SLOPING SHEAR WEB FOUND CRACKED AT FWD I/B LOWER CORNER. LEFT SLOPING SHEAR WEB REPLACED AS PER SRM 51-10-01. - [SDR UIEA200700078](https://openairdocs.org/sdr/UIEA200700078.md): Blowout Door · chafed · Feb 21, 2007 · N505MC · Boeing 7472D3B · Nacelle/Pylon, Main Frame > ENGINE NR 1 AND NR 2, RT C-DUCT BLOW OUT DOOR ASSEMBLY HAS MISSING MATERIAL AND CHAFE MARKED. REPAIRED ACCOMPLISHED AS PER EO NR 4778A093 AND FAA FORM 8110-3. - [SDR UIEA200700077](https://openairdocs.org/sdr/UIEA200700077.md): Skin · corroded · Feb 21, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Plate/Skin > FOUND CENTER TANK LOWER SKIN LOWER SURFACE FOUND CORROSION JUST ABOVE NR 1 ACM. CORROSION BLEND OUT AND HFEC INSPECTION PERFORMED AS PER BOEING SR ID NR 1-290707077-1 THRU -3 AND FAA FORM 8100-9. - [SDR UIEA200700076](https://openairdocs.org/sdr/UIEA200700076.md): Skin · scratched · Feb 21, 2007 · N505MC · Boeing 7472D3B · Fuselage Main, Plate/Skin > FOUND FUSELAGE SKIN SCRATCH FOUND AT BS 2310, S38L-S40L. SCRATCH SLIGHTLY SMOOTHED AND PROTECTED AS PER SRM 51-10-02. - [SDR UIEA200700074](https://openairdocs.org/sdr/UIEA200700074.md): Skin · corroded · Feb 20, 2007 · N505MC · Boeing 7472D3B · Wing, Plate/Skin > LEFT WING LEADING EDGE BULLNOSE FOUND CORROSION OUTBOARD OF LANDING LIGHT. PERMANENT REPAIRED ACCOMPLISHED AS PER BOEING MESSAGE 1-286780848-2 DATED 13 FEB,2007 AND EO NR 4757A281. - [SDR UIEA200700071](https://openairdocs.org/sdr/UIEA200700071.md): Stiffener · cracked · Feb 18, 2007 · N505MC · Boeing 7472D3B · Fuselage Miscellaneous Structure > FOUND UPPER DECK FLOORBEAM ONE STIFFENER CRACKED AT BS 400 LBL15. UPPER DECK FLOORBEAM STIFFENER REPLACED AS PER SRM 51-10-01. - [SDR UIEA200700072](https://openairdocs.org/sdr/UIEA200700072.md): Intercostal · cracked · Feb 18, 2007 · N505MC · Boeing 7472D3B · Fuselage Miscellaneous Structure > FOUND UPPER DECK FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 395 RBL 6. U/DECK FLOOR SUPPORT INTERCOSTAL REPLACED AS PER SRM 51-10-01. Next page: https://openairdocs.org/deregistered/N505MC-2010-11-29/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 = 'N505MC' AND deregistration_id = 'N505MC-2010-11-29' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N505MC-2010-11-29/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.