# Boeing 747-41R - Type: Aircraft model (FAA registry) - Registry code: 13848BO - Manufacturer (registry): BOEING - Model: 747-41R - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 4 ยท Turbo-fan - Seats: 490 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 1 - Page: https://openairdocs.org/model/boeing-747-41r Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft (1) - [N949SL](https://openairdocs.org/aircraft/N949SL): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2001, S/N 32745 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (16) As reported by operators and repair stations, by the model named in the report. - [SDR SRXR20160311005](https://openairdocs.org/sdr/SRXR20160311005), Mar 11, 2016: BUSHING. LOOSE. RIGHT INBD T/E FLAP, NR 5 FLAP TRACK FWD ATTACH FITTING BUSHING HAS EXCESSIVE PLAY, REPAIR WAS ACCOMPLISHED ON NRC A026298 IAW VT SAA EA 747-5750-39-A6069 I/R A - [SDR SRXR20160311004](https://openairdocs.org/sdr/SRXR20160311004), Mar 11, 2016: FRAME. CRACKED. NR 1 OTBD CORE COWL LOWER AFT END FRAME IS CRACKED. REPAIR WAS ACCOMPLISHED ON VT SAA NRC A024927 IAW VT EA 747-5445-39-A6117 I/R AND FAA APPROVED 8110-3, DATED - [SDR SRXR20160310003](https://openairdocs.org/sdr/SRXR20160310003), Mar 10, 2016: SKIN. GOUGED. L5 DOOR LOWER FWD JAMB STOP SUPPORT STRUCTURE IS GOUGED, ACCOMPLISHED REPAIR ON NRC A025042 IAW EA 747-5330-39-A6139. - [SDR SRXR20160310002](https://openairdocs.org/sdr/SRXR20160310002), Mar 10, 2016: FRAME. DAMAGED. NR 2 INBD CORE COWL LOWER MOST AFT FRAME HAD ELONGATED HOLES, REPAIR WAS ACCOMPLISHED ON VT NRC A024852 IAW EA 747-5445-39-A6116, I/R AND FAA APPROVED 8110-3 DA - [SDR SRXR20160307001](https://openairdocs.org/sdr/SRXR20160307001), Mar 7, 2016: FIRESEAL. CRACKED. NR 4 ENGINE OTBD T/R FIRESEAL RETAINER IS CRACKED, REPAIR WAS ACCOMPLISHED ON NRC A024766 IAW EA 747-5445-39-A6121 I/R AND FAA APPROVED 8110-3, DATED FEB 23 201 - [SDR SRXR2016FA0000112](https://openairdocs.org/sdr/SRXR2016FA0000112), Mar 4, 2016: WEDGE. DAMAGED. RT WINGLET T/E WEDGE WAS FOUND WITH UPPER CORNER MISSING RELATED TO HIGH VOLTAGE DISCHARGE. REPAIR WAS ACCOMPLISHED ON NRC A024409 IAW EA 747-5730-39-A6077 I/R - [SDR SRXR2016FA0000111](https://openairdocs.org/sdr/SRXR2016FA0000111), Mar 4, 2016: WEDGE. DAMAGED. RT WINGLET T/E WEDGE UPPER CORNER MISSING, RELATED TO HIGH VOLTAGE DISCHARGE. REPAIR WAS ACCOMPLISHED ON NRC A024213 IAW EA 747-5730-39-A6076 I/R AND FAA APPROV - [SDR SRXR2016FA0000110](https://openairdocs.org/sdr/SRXR2016FA0000110), Mar 4, 2016: FITTING. GOUGED. LEFT INBD MID FLAP OTBD SPHERICAL BEARING FITTING IS GOUGED AT SAFETY LINK BOLT HOLE. REPAIR WAS ACCOMPLISHED ON NRC A026329 IAW EA 747-5753-39-A6075, REV I/R A - [SDR SRXR2016FA0000109](https://openairdocs.org/sdr/SRXR2016FA0000109), Mar 4, 2016: FITTING. GOUGED. LEFT INBD FLAP, INBD SPHERICAL BEARING GOUGED AT AT SAFETY LINK BOLT HOLE. REPAIR WAS ACCOMPLISHED ON NRC A026333 IAW VT EA 747-5753-39-A6075 IR AND FAA APROVED - [SDR SRXR2016F00073](https://openairdocs.org/sdr/SRXR2016F00073), Mar 4, 2016: FITTING. GOUGED. RIGHT INBD MID FLAP OTBD SPHERICAL BEARING FITTING IS GOUGED AT SAFETY LOCK BOLT HOLE. REPAIR WAS ACCOMPLISHED IAW EA 747-5753-39-A6074 I/R AND FAA APPROVED 811 - [SDR SRXR2016F00072](https://openairdocs.org/sdr/SRXR2016F00072), Mar 4, 2016: FITTING. GOUGED. RIGHT INBD MID FLAP, INBD SPHERICAL BEARING FITTING IS GOUGED OTBD OF SAFETY LINK. REPAIR WAS ACCOMPLISHED ON NRC A026314 IAW EA 747-5753-39-A6074, REV I/R AND - [SDR SRXR2016F00069](https://openairdocs.org/sdr/SRXR2016F00069), Mar 3, 2016: FITTING. GOUGED. RIGHT INBD MID FLAP INBD SPHERICAL BEARING FITTING IS GOUGED ABOVE BEARING REF NRC A026313, REPAIR WAS ACCOMPLISHED IAW EA 747-5753-39-A6074. - [SDR SRXR2016F00068](https://openairdocs.org/sdr/SRXR2016F00068), Mar 3, 2016: BEARING. GOUGED. RIGHT INBD MID FLAP, INBD SPHERICAL BEARING FITTING IS GOUGED AT SAFETY LINK BOLT HOLE. REPAIR WAS ACCOMPLISHED IAW VT-SAA EA 747-5753-39-A6074 I/R AND FAA APPR - [SDR UALA2012042002369](https://openairdocs.org/sdr/UALA2012042002369), Apr 19, 2012: CONNECTOR. UNSECURE. MAIN GALLEY FWD & SIDE WALL EMERGENCY LIGHT INOPERATIVE. SECURED EMERGENCY LIGHT CONNECTOR. OP CHECKED NORMAL. - [SDR UALA2011042602035](https://openairdocs.org/sdr/UALA2011042602035), Apr 25, 2011: TRANSMISSION. LEAKING. NR 4 TRAILING EDGE FLAP TRANSMISSION LEAKING 7 DROPS PER MINUTE. OUT OF LIMITS. CHECK NR 4 T/E FLAP TXMSN SERVICE PER MM. WITH RESERVOIR FULL, NR 4 T/E FLAP TRA - [SDR UALA2011032101328](https://openairdocs.org/sdr/UALA2011032101328), Mar 20, 2011: LIGHT. LOOSE. EMERGENCY LIGHT LOWER SIDE OF LAV DOOR AT 2R IS LOOSE. LIGHT IS UN-SECURE. TIGHTENED SAME, SYS CHECKS GOOD. --- 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.